Thermal Response Characteristics of Flat Plate Heated by High Temperature and High Speed Flow

Article Preview

Abstract:

According to the view of heat transfer, the process of the fluid flow with high temperature and high speed over a flat plate may be considered as the heat transfer process within a compressible thermal boundary layer. Based on the numerical results of thermal isolation assumption, combining the temperature comparison with modification method, a coupled method of convection heat transfer coefficient with temperature field of the plate is established, and the characteristics of the thermal response for the flat plate is dominated. Take some ribbed plates as instances, the convection heat transfer coefficient and temperature field of the plate are simulated through the provided coupled method. The results show that, not only the position and materials of the plate influence the convection heat transfer coefficient, but also the time.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

3316-3319

Citation:

Online since:

October 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] JIANG Zhi-jie, ZHANG Bo-yi, HE Hao, et al. Research on analysis of thermal environment and structure of nose tip for hypersonic vehicle. Missile and Space Vehcile, 2009, 4: 14-18(in Chinese).

Google Scholar

[2] Dietiker J F, Hoffmann K A. Challenges in the heat transfer computations of high speed flows. AIAA, 2004: 1-10.

DOI: 10.2514/6.2004-993

Google Scholar

[3] Wassel A T, Issacci F, Griethuysen V V, et al. An integrated modeling approach for hypersonic aircraft thermal management. AIAA, 1995: 1-11.

DOI: 10.2514/6.1995-6022

Google Scholar

[4] LV Li-li, ZHANG Wei-wei, YE Zheng-yin. Prediction heating distributions for hypersonic reentry bodies. Chinese Journal of Applied Mechanics, 2006, 23(2): 259-262(in Chinese).

Google Scholar

[5] JIANG You-di, DONG Wei, CHEN Yong. Transient surface heat flux and surface temperature engineering prediction of hypersonic vehicle. Energy Technology, 2007, 28(6): 315-318(in Chinese).

Google Scholar

[6] Peter A G. Computational fluid dunamics technology for hypersonic application. AIAA, 2003: 3259.

Google Scholar

[7] Eckert E R G., Drake R M. Analysisi of heat and mass transfer. McGraw Hill, (1972).

Google Scholar

[8] Kays W M, Crawford M E, Weigand B. Convection heat and mass transfer (Fourth Edition). McGraw Hill. (2005).

Google Scholar

[9] WANG Jun, WANG Pei-guang. Integrated thermal protection and control system design methodology for hypersonic vehicles. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(10): 1129-1134(in Chinese).

Google Scholar